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Remove non-ASCII characters

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Henry
2012-01-19 16:27:23 +00:00
parent fa9eb43280
commit 0b1bcbb753
11 changed files with 28 additions and 28 deletions
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4
applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
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@ -114,11 +114,11 @@ public:
//- the dragfunction K used in the momentum eq. //- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub) // ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua) // ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB! *****************************
// for numerical reasons alpha and beta has been // for numerical reasons alpha and beta has been
// extracted from the dragFunction K, // extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function // so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0; virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
}; };

4
applications/solvers/multiphase/compressibleTwoPhaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H
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@ -114,12 +114,12 @@ public:
//- the heat-transfer function K used in the enthalpy eq. //- the heat-transfer function K used in the enthalpy eq.
// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb) // ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta) // ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB!*****************************
// for numerical reasons alpha and beta has been // for numerical reasons alpha and beta has been
// extracted from the heat-transfer function K, // extracted from the heat-transfer function K,
// so you MUST divide K by alpha*beta when implementing the // so you MUST divide K by alpha*beta when implementing the
// heat-transfer function // heat-transfer function
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB!*****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0; virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
}; };

4
applications/solvers/multiphase/interPhaseChangeFoam/phaseChangeTwoPhaseMixtures/Kunz/Kunz.H
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@ -35,8 +35,8 @@ Description
\verbatim \verbatim
Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, Lindau. J.W., Kunz, R.F., Boger, D.A., Stinebring, D.R., Chyczewski, Lindau. J.W.,
Gibeling, H.J., Venkateswaran, S., Govindan, T.R., Gibeling, H.J., Venkateswaran, S., Govindan, T.R.,
“A Preconditioned Implicit Method for Two-Phase Flows with Application "A Preconditioned Implicit Method for Two-Phase Flows with Application
to Cavitation Prediction,” to Cavitation Prediction,"
Computers and Fluids, Computers and Fluids,
29(8):849-875, 2000. 29(8):849-875, 2000.
\endverbatim \endverbatim

4
applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
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@ -131,11 +131,11 @@ public:
//- the dragfunction K used in the momentum eq. //- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub) // ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua) // ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB! *****************************
// for numerical reasons alpha and beta has been // for numerical reasons alpha and beta has been
// extracted from the dragFunction K, // extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function // so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0; virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
}; };

4
applications/solvers/multiphase/multiphaseEulerFoam/interfacialModels/heatTransferModels/heatTransferModel/heatTransferModel.H
View File

@ -114,12 +114,12 @@ public:
//- the heat-transfer function K used in the enthalpy eq. //- the heat-transfer function K used in the enthalpy eq.
// ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb) // ddt(alpha*rhoa*ha) + ... = ... alpha*beta*K*(Ta - Tb)
// ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta) // ddt(beta*rhob*hb) + ... = ... alpha*beta*K*(Tb - Ta)
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB! *****************************
// for numerical reasons alpha and beta has been // for numerical reasons alpha and beta has been
// extracted from the heat-transfer function K, // extracted from the heat-transfer function K,
// so you MUST divide K by alpha*beta when implementing the // so you MUST divide K by alpha*beta when implementing the
// heat-transfer function // heat-transfer function
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0; virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
}; };

4
applications/solvers/multiphase/twoPhaseEulerFoam/interfacialModels/dragModels/dragModel/dragModel.H
View File

@ -114,11 +114,11 @@ public:
//- the dragfunction K used in the momentum eq. //- the dragfunction K used in the momentum eq.
// ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub) // ddt(alpha*rhoa*Ua) + ... = ... alpha*beta*K*(Ua-Ub)
// ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua) // ddt(beta*rhob*Ub) + ... = ... alpha*beta*K*(Ub-Ua)
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB ! *****************************
// for numerical reasons alpha and beta has been // for numerical reasons alpha and beta has been
// extracted from the dragFunction K, // extracted from the dragFunction K,
// so you MUST divide K by alpha*beta when implemnting the drag function // so you MUST divide K by alpha*beta when implemnting the drag function
// **********************************<EFBFBD>NB ! ***************************** // ********************************** NB ! *****************************
virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0; virtual tmp<volScalarField> K(const volScalarField& Ur) const = 0;
}; };

8
src/lagrangian/molecularDynamics/molecule/reducedUnits/reducedUnits.H
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@ -76,7 +76,7 @@ class reducedUnits
scalar refPressure_; scalar refPressure_;
scalar refMassDensity_; scalar refMassDensity_;
scalar refNumberDensity_; scalar refNumberDensity_;
@ -103,9 +103,9 @@ public:
// Constructors // Constructors
//- Construct with no argument, uses default values: //- Construct with no argument, uses default values:
// length = 1nm // length = 1nm
// mass = 1.660538782e−27kg (unified atomic mass unit) // mass = 1.660538782e-27kg (unified atomic mass unit)
// temperature = 1K (therefore, energy = 1*kb) // temperature = 1K (therefore, energy = 1*kb)
reducedUnits(); reducedUnits();
//- Construct from components //- Construct from components

8
src/lagrangian/molecularDynamics/old/reducedUnits/reducedUnits.H
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@ -76,7 +76,7 @@ class reducedUnits
scalar refPressure_; scalar refPressure_;
scalar refMassDensity_; scalar refMassDensity_;
scalar refNumberDensity_; scalar refNumberDensity_;
@ -103,9 +103,9 @@ public:
// Constructors // Constructors
//- Construct with no argument, uses default values: //- Construct with no argument, uses default values:
// length = 1nm // length = 1nm
// mass = 1.660538782e−27kg (unified atomic mass unit) // mass = 1.660538782e-27kg (unified atomic mass unit)
// temperature = 1K (therefore, energy = 1*kb) // temperature = 1K (therefore, energy = 1*kb)
reducedUnits(); reducedUnits();
//- Construct from components //- Construct from components

12
src/sampling/meshToMeshInterpolation/tetOverlapVolume/tetOverlapVolume.H
View File

@ -77,10 +77,10 @@ class tetOverlapVolume
); );
//- Helping cľasses //- Helper classes
class dummyTetOp class dummyTetOp
{ {
public: public:
inline void operator()(const tetPoints&){} inline void operator()(const tetPoints&){}
}; };
@ -88,7 +88,8 @@ class tetOverlapVolume
class sumTetVolOp class sumTetVolOp
{ {
public: public:
scalar vol_; scalar vol_;
inline sumTetVolOp() inline sumTetVolOp()
@ -108,7 +109,7 @@ class tetOverlapVolume
FixedList<tetPoints, 200>& tets_; FixedList<tetPoints, 200>& tets_;
label& nTets_; label& nTets_;
public: public:
inline storeTetOp(FixedList<tetPoints, 200>& tets, label& nTets) inline storeTetOp(FixedList<tetPoints, 200>& tets, label& nTets)
: :
@ -178,7 +179,7 @@ public:
//- Destructor //- Destructor
virtual ~tetOverlapVolume(); virtual ~tetOverlapVolume();
// Public members // Public members
@ -210,7 +211,6 @@ public:
} // End namespace Foam } // End namespace Foam
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
#endif #endif

2
src/turbulenceModels/compressible/RAS/SpalartAllmaras/SpalartAllmaras.H
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@ -33,7 +33,7 @@ Description
"A One-Equation Turbulence Model for Aerodynamic Flows" "A One-Equation Turbulence Model for Aerodynamic Flows"
P.R. Spalart, P.R. Spalart,
S.R. Allmaras, S.R. Allmaras,
La Recherche A´rospatiale, No. 1, 1994, pp. 5–21. La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
Extended according to: Extended according to:

2
src/turbulenceModels/incompressible/RAS/SpalartAllmaras/SpalartAllmaras.H
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@ -33,7 +33,7 @@ Description
"A One-Equation Turbulence Model for Aerodynamic Flows" "A One-Equation Turbulence Model for Aerodynamic Flows"
P.R. Spalart, P.R. Spalart,
S.R. Allmaras, S.R. Allmaras,
La Recherche A´rospatiale, No. 1, 1994, pp. 5–21. La Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
Extended according to: Extended according to: